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TranAir: A full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations. User's manualThe TranAir computer program calculates transonic flow about arbitrary configurations at subsonic, transonic, and supersonic freestream Mach numbers. TranAir solves the nonlinear full potential equations subject to a variety of boundary conditions modeling wakes, inlets, exhausts, porous walls, and impermeable surfaces. Regions with different total temperature and pressure can be represented. The user's manual describes how to run the TranAir program and its graphical support programs.
Document ID
19950021809
Document Type
Contractor Report (CR)
Authors
Johnson, F. T. (Boeing Military Airplane Development Seattle, WA, United States)
Samant, S. S. (Boeing Military Airplane Development Seattle, WA, United States)
Bieterman, M. B. (Boeing Military Airplane Development Seattle, WA, United States)
Melvin, R. G. (Boeing Military Airplane Development Seattle, WA, United States)
Young, D. P. (Boeing Military Airplane Development Seattle, WA, United States)
Bussoletti, J. E. (Boeing Military Airplane Development Seattle, WA, United States)
Hilmes, C. L. (Boeing Military Airplane Development Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1992
Subject Category
AERODYNAMICS
Report/Patent Number
A-90092
NAS 1.26:4349
NASA-CR-4349
Funding Number(s)
CONTRACT_GRANT: NAS2-12513
PROJECT: RTOP 505-61-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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